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Oxygen gas enters a well-insulated diffuser at \(30 \mathrm{lbf} / \mathrm{in} .^{2}\), \(440^{\circ} \mathrm{R}\), with a velocity of \(950 \mathrm{ft} / \mathrm{s}\) through a flow area of \(2.0 \mathrm{in}^{2}\) At the exit, the flow area is 15 times the inlet area, and the velocity is \(25 \mathrm{ft} / \mathrm{s}\). The potential energy change from inlet to exit is negligible. Assuming ideal gas behavior for the oxygen and steady-state operation of the diffuser, determine the exit temperature, in \({ }^{\circ} \mathrm{R}\), the exit pressure, in \(\mathrm{lbf} / \mathrm{in}^{2}\), and the mass flow rate, in lb/s.

Short Answer

Expert verified
The exit temperature is 437 R, the exit pressure is 7.48 lbf/in^2, and the mass flow rate is 2.705 lbm/s.

Step by step solution

01

- Determine the mass flow rate

The mass flow rate (\textdot{m}) can be calculated using the following formula: \[ \textdot{m} = \rho \times V \times A onumber \] Where: \rho is the density of the oxygen gas at the inlet (to be determined). V is the velocity at the inlet. A is the inlet area. First, use the ideal gas law to find the density \rho at the inlet: \[\rho = \frac{P}{RT} \] Using the given data: \( P = 30 \text{ lbf/in}^2 \) \( T = 440 \text{ R}\) \( R = 48 \text{ ft} \text{ lb}_\text{f} /(\text{lb}_\text{m}\text{ R}) \) Now, convert the pressure to \( \text{ lb}_\text{f} / \text{ ft}^2 \): \[ P = 30 \text{ lbf/in}^2 \times 144 = 4320 \text{ lbf/ft}^2 \] Now find the density: \[ \rho = \frac{P}{RT} = \frac{4320 }{48 \times 440} = 0.2045 \text{ lb}_\text{m}/\text{ft}^3\] Now calculate the inlet area in square feet: \[ A_\text{in} = 2 \text{ in}^2 \times \left( \frac{1 \text{ ft}^2}{144 \text{ in}^2} \right) = 0.0139 \text { ft}^2 \] Now, find the mass flow rate: \[ \textdot{m} = 0.2045 \text{ lb}_\text{m}/\text{ft}^3 \times 950 \text{ ft/s} \times 0.0139 \text{ ft}^2 \approx 2.705 \text{ lbm/s}\]
02

- Apply the continuity equation

According to the continuity equation for steady flow, mass flow rate is conserved: \[ \textdot{m}_{in} = \textdot{m}_{out} \] So, \[ \rho_{in} V_{in} A_{in} = \rho_{out} V_{out} A_{out} \] Use the area ratio to find the exit area: \[ A_{out} = 15 \times A_{in} = 15 \times 0.0139 \text{ ft}^2 = 0.2085 \text{ ft}^2 \] Rearranging the above equation: \[ \rho_{in} V_{in} A_{in} = \rho_{out} V_{out} A_{out} \] Solving for \( \rho_{out} \): \[ \rho_{out} = \frac{\rho_{in} V_{in} A_{in}}{V_{out} A_{out}} = \frac{0.2045 \times 950 \times 0.0139}{25 \times 0.2085} \approx 0.515 \text{ lbm/ft}^3 \]
03

- Determine the exit temperature

Use the ideal gas law again to find the exit temperature: \[ \rho = \frac{P}{RT} \] Solving for \( T_{out} \): \[ T_{out} = \frac{P_{out}}{\rho_{out} R} \] But first, apply the steady-flow energy equation: \[ h_{in} + \frac{V_{in}^2}{2} = h_{out} + \frac{V_{out}^2}{2} \] For ideal gases: \[ h = c_p T \] Assuming constant specific heats: \[ c_p = 0.240 \frac{Btu}{lbm R} \approx 1.71 \text{ Btu/lbm R} onumber \] So, \[ (1.71 \times 440 + \frac{950^2}{2 \times 32.174}) = 1.71 T_{out} + \frac{25^2}{2 \times 32.174} \] Solving for \(T_{out}\): \[ 1.71 T_{out} = 924 + 14046.3 - 9.7 \] \[1.71 T_{out} = 14962.6 \] \[ T_{out} \approx 437 \text{ R} \]
04

- Determine the exit pressure

Use the ideal gas law again: \[ P_{out} = \rho_{out} R T_{out} \] Substitute the values: \[ P_{out} = 0.515 \times 48 \times 437 = 1077.9 \text {lbf/ft}^2 \] Now, convert back to lbf/in^2: \[ P_{out} = \frac{1077.9}{144} = 7.48\text {lbf/in}^2 \]

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Ideal Gas Law
The ideal gas law is a fundamental equation in thermodynamics that relates the pressure, volume, and temperature of an ideal gas. The law is expressed as:
\[ PV = nRT \]
Where:
  • P is the pressure
  • V is the volume
  • n is the number of moles of gas
  • R is the universal gas constant
  • T is the temperature in absolute terms (Rankine, Kelvin)
In this specific problem, we use a form of the ideal gas law to determine the density of the oxygen gas at the inlet:
\[ \rho = \frac{P}{RT} \]
This reformulation helps us find the mass per unit volume of the gas, which is crucial for calculating the mass flow rate.
Mass Flow Rate
Mass flow rate (\textdot{m}) is a measure of the amount of mass moving through a given area per unit time. It’s essential for analyzing systems with fluid flow. The formula used is:
\[ \textdot{m} = \rho V A \]
Where:
  • \( \rho \) is the density
  • \( V \) is the velocity
  • \( A \) is the cross-sectional area through which the fluid flows
In the problem, we calculate the mass flow rate at the inlet using the density derived from the ideal gas law, the given velocity, and the flow area. This allows us to keep track of the mass of oxygen flowing through the diffuser.
Continuity Equation
The continuity equation states that for a steady flow, the mass flow rate must remain constant from one cross-section to another in a flow system. Mathematically, it’s expressed as:
\[ \textdot{m}_{in} = \textdot{m}_{out} \]
This can be expanded to:
\[ \rho_{in} V_{in} A_{in} = \rho_{out} V_{out} A_{out} \]
By knowing the mass flow rate and the areas at both the inlet and outlet, we can use the continuity equation to find unknown quantities, such as the exit density \( \rho_{out} \). This step ensures mass conservation throughout the diffuser, vital for accurate calculations of other parameters like pressure and temperature at the exit.
Steady-Flow Energy Equation
The steady-flow energy equation is used to analyze energy changes in a thermodynamic system where fluid flows steadily. It is given by:
\[ h_{in} + \frac{V_{in}^2}{2} = h_{out} + \frac{V_{out}^2}{2} \]
For ideal gases with constant specific heats:
\[ h = c_p T \]
Where:
  • \( h \) is the specific enthalpy
  • \( c_p \) is the specific heat at constant pressure
  • \( T \) is the temperature
By plugging in the values and solving for the exit temperature \( T_{out} \), we gain insights into how the energy transformations within the diffuser affect its thermodynamic state. This calculated temperature is later used alongside the ideal gas law to derive the exit pressure.

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Most popular questions from this chapter

Oil enters a counterflow heat exchanger at \(450 \mathrm{~K}\) with a mass flow rate of \(10 \mathrm{~kg} / \mathrm{s}\) and exits at \(350 \mathrm{~K}\). A separate stream of liquid water enters at \(20^{\circ} \mathrm{C}, 5\) bar. Each stream experiences no significant change in pressure. Stray heat transfer with the surroundings of the heat exchanger and kinetic and potential energy effects can be ignored. The specific heat of the oil is constant, \(c=2 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\). If the designer wants to ensure no water vapor is present in the exiting water stream, what is the allowed range of mass flow rates for the water, in \(\mathrm{kg} / \mathrm{s}\) ?

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Air at \(600 \mathrm{kPa}, 330 \mathrm{~K}\) enters a well-insulated, horizontal pipe having a diameter of \(1.2 \mathrm{~cm}\) and exits at \(120 \mathrm{kPa}\), \(300 \mathrm{~K}\). Applying the ideal gas model for air, determine at steady state (a) the inlet and exit velocities, each in \(\mathrm{m} / \mathrm{s}\), and (b) the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\).

Steam at a pressure of \(0.08\) bar and a quality of \(93.2 \%\) enters a shell- and-tube heat exchanger where it condenses on the outside of tubes through which cooling water flows, exiting as saturated liquid at \(0.08\) bar. The mass flow rate of the condensing steam is \(3.4 \times 10^{5} \mathrm{~kg} / \mathrm{h}\). Cooling water enters the tubes at \(15^{\circ} \mathrm{C}\) and exits at \(35^{\circ} \mathrm{C}\) with negligible change in pressure. Neglecting stray heat transfer and ignoring kinetic and potential energy effects, determine the mass flow rate of the cooling water, in \(\mathrm{kg} / \mathrm{h}\), for steady-state operation.

Helium gas flows through a well-insulated nozzle at steady state. The temperature and velocity at the inlet are \(550^{\circ} \mathrm{R}\) and \(150 \mathrm{ft} / \mathrm{s}\), respectively. At the exit, the temperature is \(400^{\circ} \mathrm{R}\) and the pressure is \(40 \mathrm{lbf} /\) in. \({ }^{2}\) The area of the exit is \(0.0085 \mathrm{ft}^{2}\). Using the ideal gas model with \(k=1.67\), and neglecting potential energy effects, determine the mass flow rate, in \(\mathrm{lb} / \mathrm{s}\), through the nozzle.

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